Research Article

Method for Predicting the Liquid-Sloshing Characteristics of a Microsatellite Propulsion System

Table 24

Relative errors of calculation and simulation results for storage tank and microsatellite with the deployment mechanism.

Calculation results (°/s)Simulation results (°/s)Relative errors

1.3%
6.3%
4.2%
1.6%
4.3%
7.6%